JPH01156456A - Method for hot-working titanium ingot - Google Patents
Method for hot-working titanium ingotInfo
- Publication number
- JPH01156456A JPH01156456A JP31368287A JP31368287A JPH01156456A JP H01156456 A JPH01156456 A JP H01156456A JP 31368287 A JP31368287 A JP 31368287A JP 31368287 A JP31368287 A JP 31368287A JP H01156456 A JPH01156456 A JP H01156456A
- Authority
- JP
- Japan
- Prior art keywords
- hot
- ingot
- working
- alloy
- recrystallization
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/02—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling heavy work, e.g. ingots, slabs, blooms, or billets, in which the cross-sectional form is unimportant ; Rolling combined with forging or pressing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Metal Rolling (AREA)
- Extrusion Of Metal (AREA)
Abstract
Description
【発明の詳細な説明】
[a業上の利用分野]
本発明は、スラブあるいはビレット形状に鋳造された純
チタンあるいはチタン合金のインゴットを熱間加工し、
あるいはざらに冷間加工して板材、棒材、線材、管材、
形材等の展伸材製品を製造するに際し、インゴットの粗
大鋳造組織に起因する表面疵の発生を防止して、良好な
表面性状を有するチタン展伸材製品を製造する方法に関
するものである。[Detailed description of the invention] [Field of industrial application] The present invention involves hot working a pure titanium or titanium alloy ingot cast into a slab or billet shape,
Or roughly cold-processed into plates, bars, wires, pipes, etc.
The present invention relates to a method for manufacturing wrought titanium products having good surface properties by preventing the occurrence of surface flaws due to the coarse cast structure of an ingot when manufacturing wrought titanium products such as shapes.
[従来の技術]
純チタンおよびチタン合金の展伸材製品は、一般にVA
R(消耗電極型真空アーク溶解炉)で溶解された円柱形
のインゴットを、鍛造あるいは分塊圧延によってスラブ
やビレットに成形し、これを熱間圧延、熱間押出等の熱
間加工に供し、あるいはさらに冷間加工して製造されて
いる。しかしVAR溶解では、成分調整のため2回溶解
が必要であり、また消耗電極型であるため溶解原料とし
てのチタンスクラップの再溶解が制限されるなどの問題
がある。そこで近年、EBR(電子ビーム溶解)やVF
R(真空プラズマ溶解)等のチタンの新しい溶解法の開
発が進んでいる。これらの新しい溶解法の特長は、自由
な断面形状のインゴットが製造できることであり、スラ
ブあるいはビレット形状のインゴットを鋳造することに
より、従来の鍛造あるいは分塊圧延等のいわゆるブレー
クダウン工程を省略することが可能である。[Prior art] Pure titanium and titanium alloy wrought products generally have a VA
A cylindrical ingot melted in R (consumable electrode type vacuum arc melting furnace) is formed into a slab or billet by forging or blooming, and this is subjected to hot processing such as hot rolling or hot extrusion. Alternatively, it is manufactured by further cold working. However, VAR melting requires two melting steps to adjust the components, and since it is a consumable electrode type, there are problems such as the ability to remelt titanium scrap as a raw material for melting. Therefore, in recent years, EBR (electron beam melting) and VF
Development of new titanium melting methods such as R (vacuum plasma melting) is progressing. The feature of these new melting methods is that ingots with any cross-sectional shape can be manufactured, and by casting ingots in slab or billet shape, the so-called breakdown process such as conventional forging or blooming rolling can be omitted. is possible.
[発明が解決しようとする問題点コ
しかし、インゴットを鍛造あるいは分塊圧延を省略して
直接に熱間圧延や熱間押出などに供゛した場合には、イ
ンゴットの粗大な結晶粒と各結晶粒の変形の異方性に起
因して、表面に目視できるほどの凹凸が生じ、これが加
工率の増加に伴って割れやスジ状の表面疵となる。これ
らの熱間加工材を製品化するに際しては、表面手入れが
必要となり、大幅な歩留り低下の原因となっている。例
えば板の熱間圧延では耳割れが発生し、熱間圧延製品と
してもまた冷間圧延用素材としても、エツジトリミング
等による耳割れ部の除去が必要となる。また線の熱間圧
延材や棒の熱間押出材では表面にスジ状の疵が発生し、
酸洗や研削等の手入れが必要である。[Problems to be solved by the invention] However, when the ingot is directly subjected to hot rolling or hot extrusion without forging or blooming, the coarse grains of the ingot and each crystal are Due to the anisotropy of grain deformation, visible irregularities occur on the surface, which become cracks and streak-like surface defects as the processing rate increases. When turning these hot-processed materials into products, surface care is required, which causes a significant decrease in yield. For example, edge cracks occur during hot rolling of plates, and the edge cracks must be removed by edge trimming or the like when used as a hot rolled product or as a material for cold rolling. In addition, streak-like defects occur on the surface of hot-rolled wire materials and hot-extruded rod materials.
Care such as pickling and grinding is required.
本発明は、このようなインゴットの粗大な結晶粒に起因
するチタン製品の表面疵を防止し、良好な表面性状を有
するチタン製品を製造することを目的とする。An object of the present invention is to prevent surface flaws on titanium products caused by such coarse crystal grains of ingots, and to produce titanium products with good surface properties.
[問題点を解決するための手段・作用]そこで本発明者
等は、インゴットの表面層の組織を再結晶微細化するこ
とによって、表面疵の発生を防止する手段について検討
した結果、加熱前のインゴットに、鍛造あるいは圧延等
を施して、少なくとも表面層に加工ひずみを加え、これ
を再結晶温度以上に加熱してインゴットの少なくとも表
面層を再結晶させることにより、熱間加工時の表面疵発
生を低減することが可能であることを見出した。この際
の再結晶層の厚さは2mm以上であることが望ましく、
加工ひずみの付加手段やインゴット寸法さらに再結晶粒
径の大きさにはほとんど関係ないことを確認して本発明
に至った。[Means and effects for solving the problem] Therefore, the present inventors investigated a means to prevent the occurrence of surface flaws by recrystallizing the structure of the surface layer of the ingot. By applying processing strain to at least the surface layer of the ingot by forging or rolling, and then heating it above the recrystallization temperature to recrystallize at least the surface layer of the ingot, surface flaws can be prevented during hot working. We have found that it is possible to reduce the The thickness of the recrystallized layer at this time is preferably 2 mm or more,
The present invention was achieved by confirming that there is almost no relation to the method of applying processing strain, the ingot size, or the recrystallized grain size.
本発明では、鍛造や分塊圧延を省略することが前提であ
るため、素材として純チタンあるいは種々のチタン合金
のインゴット(スラブあるいはビレット形状)を用いた
。これらの材料の表面層にショツトブラスト、鍛造ある
いはロール圧下等による加工を加え、ついで加熱し、熱
間加工(板圧延、線材圧延、熱間押出等)を行い、表面
層の再結晶状態と表面疵発生状況を調べたところ、表面
疵の発生状況が鍛造材あるいは分塊材を熱間加工した場
合と同程度かあるいはより良好であるための条件は、素
材の成分、表面加工方法および再結晶粒径に関係なく、
表層からの再結晶層厚さは2mm以上が望ましいことが
わかった。ただし、インゴット加工時の材料温度は、加
工により表面に残留ひずみが発生する温度域であること
が必要であり、一般には再結晶温度以下である。Since the present invention is based on the premise of omitting forging and blooming, an ingot (slab or billet shape) of pure titanium or various titanium alloys was used as the material. The surface layer of these materials is processed by shot blasting, forging, roll reduction, etc., then heated, and hot processed (plate rolling, wire rolling, hot extrusion, etc.) to determine the recrystallized state of the surface layer and the surface. When we investigated the occurrence of defects, we found that the conditions for the occurrence of surface defects to be on the same level or better than when hot-processing forged or bloomed materials are the composition of the material, surface processing method, and recrystallization. Regardless of particle size,
It was found that the thickness of the recrystallized layer from the surface layer is preferably 2 mm or more. However, the material temperature during ingot processing needs to be in a temperature range where residual strain occurs on the surface due to processing, and is generally below the recrystallization temperature.
[実 施 例]
実施例−1
厚さ60mm、幅1100mmのスラブに鋳造した純チ
タンJIS2種およびチタン合金(Ti−5A1−2.
5 Sn)のインゴットの側面を、片面の幅減少量で1
mm、2mm、3mmおよび5mmの鍛造を行った。[Example] Example-1 Pure titanium JIS Class 2 and titanium alloy (Ti-5A1-2.
5 Sn) The side of the ingot is reduced by 1 by the amount of width reduction on one side.
Forging of mm, 2mm, 3mm and 5mm was performed.
鍛造は、純チタンは常温(約30℃)で、またチタン合
金は常温および油浴中で約200℃に加熱した後に行っ
た。該スラブを純チタンは加熱温度860℃、圧下率9
8%、チタン合金は加熱温度1150℃、圧下率96%
で各々熱間圧延した。Pure titanium was forged at room temperature (approximately 30° C.), and titanium alloys were forged at room temperature and after being heated to approximately 200° C. in an oil bath. The slab was made of pure titanium at a heating temperature of 860°C and a reduction rate of 9.
8%, titanium alloy heating temperature 1150℃, reduction rate 96%
Each was hot rolled.
また比較として、鋳造ままのスラブとこれを熱間鍛造し
たスラブも同様に熱間圧延した。これらについてスラブ
表層の再結晶層厚さと、熱間圧延材の耳割れについて調
べた結果を表1に示す。熱間圧延まえに鍛造を行いスラ
ブ側面を再結晶させることで、熱間圧延材の耳割れ発生
は低減されることがわかる。そして純チタンでは、表面
に厚さ2mm以上の再結晶層を生成させることにより、
製品として全く問題のない表面性状のものが得られた。For comparison, an as-cast slab and a hot-forged slab were similarly hot-rolled. Table 1 shows the results of investigating the thickness of the recrystallized layer on the surface of the slab and the edge cracking of the hot rolled material. It can be seen that by forging and recrystallizing the side surfaces of the slab before hot rolling, the occurrence of edge cracks in the hot rolled material can be reduced. And with pure titanium, by creating a recrystallized layer with a thickness of 2 mm or more on the surface,
A product with a surface quality without any problems was obtained.
またチタン合金では、表面に厚さ2mm以上の再結晶層
を生成されることにより耳割れ発生は従来材と同程度に
なり、熱間圧延後のトリミングによる歩留り低下も従来
材と同等に抑えることができた。In addition, with titanium alloy, a recrystallized layer with a thickness of 2 mm or more is generated on the surface, so the occurrence of edge cracking is the same as that of conventional materials, and the yield loss due to trimming after hot rolling can be suppressed to the same level as conventional materials. was completed.
表 1
実施例−2
一辺り50m■の角ビレットに鋳造した純チタンJTS
2種およびチタン合金 (Tl−6Al−4V)ツイン
ゴツトの表面を、片面の幅減少量でII、2mm、3m
mおよび5mmの鍛造を行った。鍛造は、純チタンは常
温(約30℃)で、またチタン合金は常温および油浴中
で約200℃に加熱した後に行った。該ビレットを純チ
タンは加熱温度820℃、減面率98%、チタン合金は
加熱温度1150℃、減面率98%で各々熱間で線材圧
延した。また比較として、鋳造のままのビレットとこれ
を熱間で分塊圧延したビレットも同様に熱間で線材圧延
した。これらについてビレット表層の再結晶層厚さと、
熱間圧延材の表面疵深さについて調べた結果を表2に示
す。熱間圧延まえに鍛造を行いビレット表面を再結晶さ
せることにより、熱間圧延材の表面疵発生は低減される
ことがわかる。さらに厚さ2a+m以上の再結晶層を生
成させることにより、製品として全く問題のない表面性
状のものが得られた。Table 1 Example-2 Pure titanium JTS cast into a square billet with a length of 50m
The surface of the 2nd type and titanium alloy (Tl-6Al-4V) twin got is
Forging of 5 mm and 5 mm was performed. Pure titanium was forged at room temperature (approximately 30° C.), and titanium alloys were forged at room temperature and after being heated to approximately 200° C. in an oil bath. The billet was hot wire-rolled at a heating temperature of 820°C and an area reduction rate of 98% for pure titanium, and at a heating temperature of 1150°C and an area reduction rate of 98% for the titanium alloy. For comparison, an as-cast billet and a hot blooming billet were similarly hot rolled into wire rods. Regarding these, the thickness of the recrystallized layer on the billet surface layer,
Table 2 shows the results of investigating the depth of surface flaws in hot rolled materials. It can be seen that by forging and recrystallizing the billet surface before hot rolling, the occurrence of surface flaws in the hot rolled material is reduced. Furthermore, by producing a recrystallized layer with a thickness of 2 a+m or more, a product with a surface quality that was completely acceptable was obtained.
表 2
実施例−3
直径170mmの丸ビレットに鋳造した純チタンJIS
2f!i及びチタン合金 (Ti−6ALl−4V)ツ
インゴツトの表面を、外径100mmのロールで周方向
に圧下荷重1 ton、 3 ton、5 tonおよ
び8 tonで常温(約30℃)にて圧延加工した。該
ビレットを、純チタンは加熱温度920℃、減面率98
%、チタン合金は加熱温度960t、減面率84%で各
々熱間押出した。また比較として、鋳造ままのビレット
とこれを熱間で分塊圧延したビレットも同様に熱間押出
した。これらについてビレット表層の再結晶層厚さと、
熱間押出材の表面疵深さについて調べた結果を表3に示
す。Table 2 Example-3 Pure titanium JIS cast into a round billet with a diameter of 170 mm
2f! The surface of the titanium alloy (Ti-6ALl-4V) twingots was rolled at room temperature (approximately 30°C) with rolling loads of 1 ton, 3 ton, 5 ton, and 8 ton in the circumferential direction using rolls with an outer diameter of 100 mm. . For pure titanium, the billet was heated at a heating temperature of 920°C and an area reduction rate of 98.
% and titanium alloys were hot extruded at a heating temperature of 960 t and an area reduction rate of 84%. For comparison, an as-cast billet and a billet obtained by hot blooming were also hot extruded. Regarding these, the thickness of the recrystallized layer on the billet surface layer,
Table 3 shows the results of investigating the depth of surface flaws in hot extruded materials.
熱間押出まえに圧延加工を行いビレット表面を再結晶さ
せることにより、熱間押出材の表面疵発生は低減される
ことがわかる。さらに厚さ2mm以上の再結晶層を生成
されることにより、製品として全く問題のない表面性状
のものが得られた。It can be seen that by performing rolling to recrystallize the billet surface before hot extrusion, the occurrence of surface flaws in the hot extruded material is reduced. Furthermore, by producing a recrystallized layer with a thickness of 2 mm or more, a product with a surface quality that had no problems at all was obtained.
表 3
[発明の効果]
上述のように、本発明によれば従来、組織微細化のため
必要であった鍛造あるいは分塊圧延を省略して、粗大な
組織を有する純チタンあるいはチタン合金のインゴット
を直接熱間加工に供して、良好な表面性状を有する製品
を得ることが可能であり、工程省略による利益には犬な
るものがある。Table 3 [Effects of the Invention] As described above, according to the present invention, it is possible to omit the forging or blooming rolling that was conventionally necessary to refine the structure, and to produce an ingot of pure titanium or titanium alloy having a coarse structure. It is possible to obtain a product with good surface properties by directly subjecting it to hot processing, and the benefits of skipping the process are significant.
Claims (1)
ひずみを加えた後、再結晶温度以上に加熱して表面層の
組織を再結晶させ、続いて熱間加工を行うことを特徴と
するチタンインゴットの熱間加工方法。Thermal processing of titanium ingots is characterized by applying processing strain to the surface layer of a pure titanium or titanium alloy ingot, then heating it above the recrystallization temperature to recrystallize the structure of the surface layer, followed by hot working. Inter-processing method.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP31368287A JPH01156456A (en) | 1987-12-11 | 1987-12-11 | Method for hot-working titanium ingot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP31368287A JPH01156456A (en) | 1987-12-11 | 1987-12-11 | Method for hot-working titanium ingot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01156456A true JPH01156456A (en) | 1989-06-20 |
Family
ID=18044244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP31368287A Pending JPH01156456A (en) | 1987-12-11 | 1987-12-11 | Method for hot-working titanium ingot |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01156456A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010090352A1 (en) | 2009-02-09 | 2010-08-12 | 新日本製鐵株式会社 | Titanium material for hot rolling and manufacturing method thereof |
| CN104174807A (en) * | 2013-05-22 | 2014-12-03 | 咸阳天成钛业有限公司 | Manufacturing method of large-caliber thick-walled titanium tube block |
| CN106425317A (en) * | 2016-11-15 | 2017-02-22 | 宝钛集团有限公司 | Preparation method of Ti-B19 high-strength titanium alloy large-caliber thick wall pipe |
| KR20170046704A (en) | 2014-09-30 | 2017-05-02 | 신닛테츠스미킨 카부시키카이샤 | Cast titanium slab for use in hot rolling and unlikely to exhibit surface defects, and method for producing same |
| JP2018001249A (en) * | 2016-07-06 | 2018-01-11 | 新日鐵住金株式会社 | Method for producing titanium blank for hot rolling |
| KR20180030122A (en) | 2015-07-29 | 2018-03-21 | 신닛테츠스미킨 카부시키카이샤 | Titanium material for hot rolling |
| CN109072390A (en) * | 2016-04-22 | 2018-12-21 | 奥科宁克公司 | The improved method of titanium products for finishing through squeezing out |
| CN112845648A (en) * | 2020-12-23 | 2021-05-28 | 西部新锆核材料科技有限公司 | Preparation method of titanium or titanium alloy extrusion rolling thin-wall section |
| CN115151351A (en) * | 2020-01-21 | 2022-10-04 | 日本制铁株式会社 | Manufacturing method of titanium processed material |
| CN115210010A (en) * | 2020-01-21 | 2022-10-18 | 日本制铁株式会社 | Method for manufacturing processed titanium material |
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|---|---|---|---|---|
| JPS60230968A (en) * | 1984-04-27 | 1985-11-16 | Nippon Mining Co Ltd | Manufacture of rolled titanium alloy plate |
| JPS61253354A (en) * | 1985-05-07 | 1986-11-11 | Nippon Kokan Kk <Nkk> | Manufacture of alpha+beta type titanium alloy sheet |
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1987
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS60230968A (en) * | 1984-04-27 | 1985-11-16 | Nippon Mining Co Ltd | Manufacture of rolled titanium alloy plate |
| JPS61253354A (en) * | 1985-05-07 | 1986-11-11 | Nippon Kokan Kk <Nkk> | Manufacture of alpha+beta type titanium alloy sheet |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010090352A1 (en) | 2009-02-09 | 2010-08-12 | 新日本製鐵株式会社 | Titanium material for hot rolling and manufacturing method thereof |
| CN102307682A (en) * | 2009-02-09 | 2012-01-04 | 新日本制铁株式会社 | Titanium billet for hot rolling and its manufacturing method |
| JP4990398B2 (en) * | 2009-02-09 | 2012-08-01 | 新日本製鐵株式会社 | Titanium material for hot rolling and manufacturing method thereof |
| RU2486973C2 (en) * | 2009-02-09 | 2013-07-10 | Ниппон Стил Корпорейшн | Titanium material for hot rolling and method of its production |
| KR101354948B1 (en) * | 2009-02-09 | 2014-01-22 | 도호 티타늄 가부시키가이샤 | Titanium material for hot rolling and manufacturing method therefof |
| US8709178B2 (en) | 2009-02-09 | 2014-04-29 | Nippon Steel & Sumitomo Metal Corporation | Titanium material for hot rolling and method of producing the same |
| CN105834215A (en) * | 2009-02-09 | 2016-08-10 | 新日铁住金株式会社 | Titanium material for hot rolling and method of producing the same |
| CN104174807A (en) * | 2013-05-22 | 2014-12-03 | 咸阳天成钛业有限公司 | Manufacturing method of large-caliber thick-walled titanium tube block |
| US11504765B2 (en) | 2014-09-30 | 2022-11-22 | Nippon Steel Corporation | Titanium cast product for hot rolling unlikely to exhibit surface defects and method of manufacturing the same |
| KR20170046704A (en) | 2014-09-30 | 2017-05-02 | 신닛테츠스미킨 카부시키카이샤 | Cast titanium slab for use in hot rolling and unlikely to exhibit surface defects, and method for producing same |
| US10913242B2 (en) | 2015-07-29 | 2021-02-09 | Nippon Steel Corporation | Titanium material for hot rolling |
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| CN115151351A (en) * | 2020-01-21 | 2022-10-04 | 日本制铁株式会社 | Manufacturing method of titanium processed material |
| CN115210010A (en) * | 2020-01-21 | 2022-10-18 | 日本制铁株式会社 | Method for manufacturing processed titanium material |
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